Journal of Space Science and Technology

Journal of Space Science and Technology

Journal of Space Science and Technology

Journal Archive

Journal of Space Science and Technology is an open access double-blind peer-reviewed quarterly journal, owned, managed and published by IAS since 2008. The journal publishes original and high-quality peer-reviewed papers containing significant results relevant to all aspects of Space System Engineering, Space Operation and Applications, Commerce, Management, Space Law, Space Sciences and Exploration and Investigating Space Radiation.

Journal Title

 Journal of Space Science and Technology

P-ISSN

 2008-4560

E-ISSN

 2423-4516

Frequency

 Quarterly

Editor-in-Chief

 Reza Ebrahimi, Ph.D.

Language 

 Persian with English Abstracts

Plagiarism Checker

 Hamanandjo, iThenticate

Peer Review Policy

 Double-blind

Article Processing Charges

 No APC (Free)

Average Review Time

 3 Months

Acceptance Rate

 30%

Owner & Publisher

 ARI, IAS

The Journal of Space Science and Technology is now accepting original research papers in English also featuring a swift review prosses

          

 

Most Visited Articles
Physical Initial Flight Alignment for Stabilized Platform Inertial Navigation System Using State Feedback
Free Vibration Analysis of Grid Stiffened Doubly Curved Composite Shells Using a Refined Higher Order Theory
Scientometric Analysis of Published Scientific Productions in the Field of Satellite Constellations
A Review on Underactuated Attitude Control of Reaction Wheel Actuated Satellites
Research Trends in Utilizing Artificial Intelligence in Satellite-Based Internet of Things: A Scientometric Analysis
GPS-RTK Integrated with Micro-Electro Mechanical INS for Precise Application
Performance Analysis of FMC Actuators to Microsatellite Temperature Management Based on 3-Axis and Pyramidal Configuration
Current Issue: Volume 19, Issue 3, 2026 

Machine Learning–Driven Prediction of the S4 Scintillation Index and Geomagnetic Storms using GNSS-RO Data

Pages 13-29

10.22034/jsst.2025.1585

Delaram Fattahi, Sahar Barzegar, Masoud Khoshsima, Saber Karami, Hadi Jalili, Jamal Aghayari

Keywords Cloud

  • Attitude control
  • satellite
  • Genetic Algorithm
  • optimization
  • Conceptual design
  • Uncertainty
  • Reaction wheel
  • Space Radiation
  • system design
  • numerical simulation
  • Microgravity
  • Satellite attitude control
  • Remote Sensing
  • Simulation
  • Launch Vehicle
  • Spacecraft
  • Optimal control
  • Kalman Filter
  • Multidisciplinary design optimization
  • GPS
  • Satellite Constellations
  • Sounding rocket
  • Swirl injector
  • Optimal guidance
  • Reliability
  • Nozzle
  • Extended Kalman Filter
  • Monopropellant thruster
  • CubeSat
  • Thruster
  • Attitude determination
  • Reaction wheels
  • Air bearing
  • Guidance law
  • Pitch program
  • Liquid Propellant Engine
  • remote sensing satellite
  • guidance
  • TLE
  • Stability Analysis
  • Outer space
  • Sensitivity analysis
  • Inertial Navigation System
  • Helmholtz coil
  • Star tracker
  • Finite Element
  • Saturation
  • flexible spacecraft
  • heat transfer
  • Machine Learning
  • star sensor
  • fault detection
  • attitude estimation
  • Low thrust
  • Sliding mode control
  • LEO satellite
  • INS
  • atomization
  • Aerodynamic heating
  • Sovereignty
  • Geostationary orbit
  • manned spacecraft
  • Microstructure
  • Magnetorquer
  • Numerical analysis
  • Design optimization
  • Magnetometer
  • Radiation
  • Electrical power subsystem
  • Reentry
  • Solar Cell
  • Fuzzy logic
  • Model predictive Control
  • Displacement damage
  • Space Capsule
  • Star catalog
  • Transverse flow
  • Calibration
  • GEO satellite
  • Inertial Navigation
  • Positioning
  • Neural Network
  • Modeling
  • Spray cone
  • Hypersonic Flow
  • Ground station
  • Integrated Navigation
  • spacecraft formation flying
  • Robust Control
  • vibration
  • State dependent riccati equation
  • LQR
  • time series
  • Sliding mode
  • launcher
  • Catalyst
  • Terminal sliding mode
  • Composite
  • image processing
  • Space
  • Proportional navigation
  • Microsatellite
  • Sun sensor
  • Hydrogen peroxide
  • cryogenic
  • Space law
  • Numerical modeling
  • Artificial Neural Network
  • Responsibility
  • design requirements
  • Integrated guidance and control
  • EKF
  • Radiation damage
  • orbital mechanics
  • Solid Rocket Motor
  • Magnetic attitude control
  • decomposition chamber
  • IMU
  • design algorithm
  • Fault Isolation
  • Orbit Determination
  • heat flux
  • simulator
  • growth
  • Orbital maneuver
  • Capillary injector
  • Plasma antenna
  • Stereo
  • Nanosatellite
  • Combustion chamber
  • Starlink
  • Quantitative feedback theory
  • UDF
  • Cost
  • Required velocity
  • GDOP
  • Monopropellant
  • Magnetic field
  • CanSat
  • Satellite remote sensing
  • Thrust vector control
  • Satellite subsystems
  • Neural Networks
  • Artificial Neural Networks
  • Recursive least squares
  • Turbulent Flow
  • thermal control
  • solar array
  • Cold gas thruster
  • Fault-tolerant control
  • imaging payload
  • Antenna Pointing Mechanism
  • Uncertainty and actuator saturation
  • Shooting Method
  • gimbal control moment gyro
  • Reconfiguration
  • LEO
  • Non-interfering architecture
  • STK software
  • TEC
  • Collaborative design
  • Initial alignment
  • Bipropellant propulsion system
  • Propulsion System
  • separation system
  • optimal trajectory
  • prediction
  • State control
  • Primary breakup
  • Deep Learning
  • Sloshing
  • Space weather
  • Sun simulator
  • Asteroid Apophis
  • Launch abort system
  • Position determination
  • integration
  • Gyro calibration
  • Positioning System
  • Space Traffic Management
  • redundancy
  • Thrust
  • Flexible satellite
  • Adaptive attitude control
  • breast cancer
  • Communication satellite
  • linear Instability
  • Attitude determination and control subsystem
  • Optimized environment
  • LEO Orbit
  • Space industry
  • Pulse-Width Pulse-Frequency Modulator
  • upper stage
  • HZETRN
  • space launch vehicle
  • payload
  • GEANT4
  • Visual Navigation
  • Control Allocation
  • space structures